Inertial Satellite Compensation of Trajectory Instabilities of Optoelectronic Positioning Systems on a Swinging Base

This paper is devoted to the problem of increasing the accuracy of measuring of flight paths of aircraft using optoelectronic systems (OES) in sea conditions. In such conditions, it is necessary to determine and compensate for the trajectory instabilities caused by the swinging base of the OES. It is proposed to determine and compensate for these instabilities using an inertial-satellite navigation system. The problems arising from this and their solutions are considered. The results of seminatural studies are presented.